In 1952 studies were started to design a replacement for Saab Draken. "Project 1357" in 1954, was the first to have a canard layout (lots of other layouts were studied as well). I n 1961, P&W JT8D-22 was the chosen engine to be locally built, with a locally designed afterburner and lots of material changes in the rest. In 1962 the design was frozen, and the prototype first flew in Feb 8:th 1967. During the 1960's, it was foreseen that the Swedish air force would purchase 800+ Viggens, but the final figure ended up at 329.
In order to make the airframe smaller, it was early decided to replace the navigator with a good navigational computer. It's designed to withstand 12 G, but the limit in operation is 7 G.
The seat in angled back 19 degrees.
Emergency power is supplied by a ram air turbine just before the
left wing leading edge, which extends automatically on hydraulic
power failure, and just before touch down. (Earlier, it was also
always deployed whenever the landing gear was down.)
The canard doesn't contribute much lift in itself during normal flight, it acts more as a gigantic vortex generator for the main wing. During low speed flight, its rear edge flap can be lowered to increase lift and permit a high nose angle.
The requirement was that the aircraft would be able to operate from 500 m runways. A short take-off run is possible due to the powerful engine (then, it was the most powerful installed in a fighter).
Landing distance is reduced by several means: The HUD is used as a precision landing aid, making it possible to aim just 30 m in from the threshold; The landing gear thinks a landing sink rate of 5 m/s is normal, so landings are done without any flare; The thrust reverser is interconnected with the nose gear link, so it can be selected in the air and will operate when the nose is lowered. (It is not intended to be used in the air.)
The aircraft must be servicable very quickly by concripts with relatively short training. Re-fueling and re-arming by 7 men, of which 6 are concripts, must take less than 10 min for the JA 37 Viggen. The time limits for reconnaissance and attack configured aircraft are 15 and 20 minutes.
It is said that attack squadrons expect to fly 11 missions per aircraft and 24-hour period.
Designations A, Attack = Strike Sk, Skol = Training SF, Spaning Foto = Reconnaissance Photo SH, Spaning Havsövervakning = Reconnaissance Maritime surveillance J, Jakt = Fighter When two or more designations are combined, the first denotes primary role.
AJ 37 ViggenThis is the strike variant. When it was designed, guns were definitely passé, so there was no provision made for an internal cannon. Dumb bombs weren't popular either, so during the preliminary design stages, the only armament considered were missiles. It wasn't until the prototypes were actually in progress of beeing built, that someone thought of incorporating wiring for iron bombs, presumably as it was realised the HUD/Weapons Aiming Computer system would enable them to be dropped with good precision.
Main armament for the anti-shipping role, a very important role, is the Saab 304 rocket-powered anti-ship missile. For ground attack, 135 mm Bofors M70 rockets (either 21 kg GP warhead with 3.7kg explosive or 20 kg AP fragmentation warhead with 5 kg explosive) in pods of six each, were together with the command controlled, smoke-less liquid fuel Saab 305 missile, the main weapons, with the 120 kg bombs and 30 mm podded guns used when appropriate.
The Saab 305/Rb 05 missile is now an all round weapon, as it is rather effective against slow, large aircraft and helicopters too. A TV version was contemplated as the Rb 05B, but it was cheaper to buy Mavericks instead.
It has always had a secondary fighter role, with Sidewinders and 30 mm cannon in pods.
In service, it replaced the A 32A Lansen.
Sk 37 ViggenTo make room for the second cockpit, fuel and avionics was removed, so it has a shorter range and lacks a radar. The fin is taller. The rear cockpit has two periscopes to give forward vision.
The trainer version wasn't planned from the outset, as it was
considered enough for pilots to learn to fly delta winged
aircraft on Draken trainers.
To replace J 32E Lansens in the ECM role, ten two seat Viggens will be modified for that role and designated SK 37E. The first of them will be delivered late in 1998.
Apart from the [aggressor squadron] ECM role, they will be used for conversion training and be based at the F 4 wing at Östersund, where the SK 37s transferred after the F 15 wing was disbanded.
About it at F 4's web site: SK 37E Viggen - text in Swedish, but there's photos of the equipment.
SH 37 ViggenDuring the early design process, it was envisioned to have both cameras and radar in the same airframe, but that proved to take up too much space, so separate versions had to be developed.
The radar has better range than AJ 37, as well as a recorder.
A long focal length forward looking SKa 24D-600 is semi-permanently mounted on the right fuselage station, to register what's been seen on the radar and to take other photos.
During a period the wing F 13 used two Recon/Optical CA-200 1676 mm cameras inside rebuilt centre line fuel tanks.
In service it replaced the S 32C Lansen
The fuselage pylons look like this As compared to this on the attack on the recce versions and fighter version / | \ / | \ / | \ | | |
SF 37 Viggen
All fixed cameras are carried in the nose, that lacks a radar.
There are three SKa 24C-120 for horizon-to-horizon coverage, an
SKa 24-57 for wide angle pictures and two SKa 31-600 for high
altitude or stand off photography. There is also an IR-linescan
designated VKA 702.
For night photography, a pod is carried on the left fuselage
station, with three SKa 34-75 cameras loaded with IR sensitive
film in the front. The rear of the pod houses electronic IR
flashes, as does a complementary pod on the starboard fuselage
station.
In service it has replaced the S 35E Draken.
JA 37 JaktviggenBy the time this version was in final design, it was clear that guns were definitely useful, so it was given the most powerful cannon a fighter has had, a 30 mm Oerlikon KCA with 150 rounds. Rate of fire is 22.5 0.36 kg rounds/s at 1050 m/s, which gives them six times more kinetic energy than the 30 mm Adens on the attack version.
A unique feature is the coupling of the radar gunsighting mode to the autopilot, introduced with Edit 32. When the pilot places a target in a capture window, the autopilot takes over pitch and yaw, and presents bank information on the HUD for the pilot to follow. Even if it's not followed, the pitch and yaw channels have enough authority to precision aim the cannon, reducing pilot workload letting him or her concentrate on tactics and situational awareness.
The fighter version has an inertial navigation system instead of
the earlier versions' doppler navigation system. It is 13 cm
longer, partly because the RM8B engine,
which is smokeless, more powerful and better suited to high altitude
than the RM8A which powers the other Viggen versions,
is 8 cm longer than the
RM8A. There is a three stage fan, three
stage LP compressor and a seven stage HP compressor, as compared
to 2/4/7 on RM8A.
The fin is the same tall one as on Sk 37 to compensate for the longer fuselage. The external tank is the same size as on the other versions, but because there's a bulge where the gun is installed, there is no room for the abbrevited top fin of the tank, instead of three fins, this tank has four fins, in a flattened 'X'.
In spite of having a strengthened wing, an engine 100 kg heavier (2200 kg) and a fixed cannon, it only has an empty weight 400 kg more than earlier versions.
In service it has replaced and supplemented the J 35 Draken.
The system has gone through numerous upgrades since service entry. The radar is able to track more targets now, than at service entry, for example. (In the late 1980's it was revealed that the capability to track two target while scanning had been introduced, and hinted at that as hardware got cheaper, more was a strong possibility.)
The lastest software upgrade, EDIT 34, enables the JA 37 to use AMRAAM missiles. A trials aircraft started flying with it in the autumn of 1997.
This modification package, called "D", also requires some hardware updates to the aircraft, is being introduced in series aircraft from the summer of 1998, and apart from the AMRAAM compatibility also includes a weapons interface like Gripen's, the new radio TARAS, improved cockpit and computers as well as ECM. Upgrade of simulators is also included.
Edit 32, in 1993, mainly introduced advances in the flight control system and radar. Many of the hardware advances needed for Edit 32, "Modification package C", were introduced at the same time as Edit 30, in 1990, but not put to full use. One example is the upgraded radar signal processor, which now has much better ECCM, among other things.
Mod D includes the ability to carry the Ericsson
Saab Avionics U95 countermeasures pod.
One other radar function added with Edit 32 is the possibility to generate virtual targets. Saves money as some exercises can be done with fewer aircraft, but also allows exercises which from a safety standpoint would be unsuitable during peace time training.
One flight control improvment is a better autothrottle, which now behaves "more like a pilot would" and also takes into account more aircraft parameters.
Starting in 1992, 115 AJ, SF and SH 37 Viggens were rebuilt to AJS 37 standard.
One reason for the upgrade is
to take advantage of the weapons, specifically the
RBS 15F anti-ship missile and
Mjölner
bomblet dispenser, already
ordered and in production for Gripen, it was decided to
modify a number of earlier Viggens, to make
them truly multi-role.
The modification will be in two stages, the ability to carry AIM-9Ls didn't arrive until 1996.
Not all AJ/SH/SF were modified, as there was no life extension involved, and the first AJ 37s were retired soon after Gripen entered service.
"Ex AJ 37" AJS 37s were never meant to carry cameras, but will
perform radar reconnaissance missions. Initial plans were
ambitious, but for economic reasons the SF 37s weren't
modified to fulfil the ground attack role, and the radar related
hardware (switches, displays) in the AJ and SH 37s will remain as
before the modification, so each subvariant of AJS 37 got its
own designation:
AJ 37 -> AJS 37
SH 37 -> AJSH 37
SF 37 -> AJSF 37
Retired Viggens have been scrapped at Ängelholm since 1993. By mid-2000 about 100, including ten JA 37s had been scrapped.
Scrapping an AJ/S 37 takes four weeks, the more technically advanced JA 37 six weeks, as it's done carefully in order to use as much as possible for spare parts. Of the electronic parts taken out of a JA 37, up to 80% is in use in another aircraft within a month, and for example the backup artificial horizon gyro can be used in SK 60, but not only electronics is reused.
The Swedish air force has two units for international missions, Swedish Air Force Rapid Reaction Unit C-130 and AJS 37.
The AJS 37 unit consists of AJSF 37 Viggens and its mission will be photo reconnaissance in conflict areas. Currently (2000) it can be operational 90 days after decision, by 2001 it will be available in 30 days, and a planning group will be able to leave Sweden within 15 days to make preparations.
In 2004 the unit was replaced by a JAS 39 Gripen unit.
Armament options
Photo shows
AJ 37 Viggen with 120 kg bombs loaded, Rb 05 missile (green)
Rb 04E (black and white), 30 mm gun pods and 135 mm rocket pods.
Diagram shows all weapon load alternatives for
AJ 37 Viggen cleared for use in 1979.
|
|
____/n\____
_______[(.)]_______
8 6 4 2 1 3 5 7 9 The stations are numbered thus
AJ 37
T External tank (1400? litre)
R R R R 6 x 135 mm M70 rockets (364 kg)
B B B B 4 x 120 kg M63FFV fragmentation bombs, Sprängbomb m/71 Virgo
I I I I 4 x 80 kg illumination flares
04 04 04 Rb 04E, Saab 304, 620 kg rocket anti-ship missile
U22 Erijammer 200 ECM pod (350 kg) (Previously known as KA,
for "pod type A")
KB BOX-9 chaff/flare dispenser (325 kg) (KB = "pod type B")
75 75 Rb 75/75T Maverick. 75 = AGM-65A, 210 kg, 75T (T for "heavy") = AGM-65A with blast warhead, 295 kg.
05 05 Rb 05, Saab 305 command controlled missile (305 kg)
usable against ground and slow air targets
G G 30 mm Aden cannon with 150 rounds (364 kg)
24 24 Rb 24/24J Sidewinder
28 28 RB 28 Falcon (IR). The initial AAM selected for Viggen. Not used
because its long warm up period. The pylon not used because a missile
there causes too much vibration on an AJ 37. (Stations 8/9 not normally used
on AJ/S 37 due to the vibration issue.)
AJS 37
24 24 24 24 24 24 Rb 24/24J Sidewinder
74 74 74 74 Rb 74 (AIM-9L) Sidewinder (1996 and later)
15 15 Rb 15F jet powered anti-ship missile (598 kg)
BK BK BK BK Bombkapsel m/90, Mjolner. Gliding bomblet dispenser.
75 75 75 75 Rb 75 (AGM-65) Maverick (210 kg)
05 05 05 05 Rb 05, command controlled missile (305 kg)
G G 30 mm Aden cannon with 150 rounds (364 kg)
R R R R 6 x 135 mm M70 rockets (364 kg)
B B B B 4 x 120 kg M63FFV fragmentation bombs
I I I I 4 x 80 kg illumination flares
TSA TSA "Heavy guided stand-off weapon" (none selected or included in the budget
although something in the GBU-15 class was envisioned already in the
early 1980's).
R R 24 R Note that assymetric loads like can be used
-----
SK 37 Lacks a radar, so its weapons are limited to:
T External tank
R R R R 6 x 135 mm M70 rockets (364 kg)
G G 30 mm Aden cannon with 150 rounds (364 kg)
SK 37E
U95 ECM pod, not certain if this and the U22/A can be under either wing
U22/A ECM pod
KB KB Chaff and flare dispenser
BT 53 Saab BT-53 laser reflector
-----
SH 37
T External tank
FC Forward looking 600 mm camera in
U22 Erijammer 200 ECM pod (350 kg)
KB BOX-9 chaff/flare dispenser (325 kg)
24 Rb 24/24J Sidewinder
C C Port station: 3 IR film cameras, electronic IR flashes
in the rear, starboard IR flashes only.
04 04 Rb 04E, 620 kg rocket powered anti-ship missile
AJSH 37
24 24 24 24 24 24 Rb 24J Sidewinder
74 74 74 74 Rb 74 (AIM-9L) Sidewinder (1996 and later). Air cooled.
15 15 Rb 15F jet powered anti-ship missile (598 kg)
BK BK BK BK Bombkapsel m/90, Mjolner. Gliding bomblet dispenser.
G G 30 mm Aden cannon with 150 rounds (364 kg)
R R R R 6 x 135 mm M70 rockets (364 kg)
B B B B 4 x 120 kg M63FFV fragmentation bombs
I I I I 4 x 80 kg illumination flares
( TSA TSA Tungt Styrt Attackvapen = "Heavy guided stand-off weapon"
Not yet funded for Gripen, so won't be used on Viggen)
-----
SF 37
T External tank
C C Port station: 3 IR film cameras, electronic IR flashes
in the rear, starboard IR flashes only.
U22 Erijammer 200 ECM pod (350 kg)
KB BOX-9 chaff/flare dispenser (325 kg)
24 24 Rb 24/24J Sidewinder
AJSF 37
24 24 24 24 24 24 Rb24/Rb 24J Sidewinder
74 74 74 74 Rb 74 (AIM-9L) Sidewinder (1996 and later)
-----
JA 37
Built in 30 mm Oerlikon KCA with 150 rounds
T External tank, with four fins
24 24 24 24 24 24 Rb 24J Sidewinder
74 74 74 74 74 74 Rb 74 (AIM-9L) Sidewinder
71 71 Rb 71 SkyFlash
R R R R 6 x 135 mm M70 rockets (364 kg) for ground attack
F F BOY 401 flare launcher (12x2 each) Countermeasures dispensers
JA 37D
C C BOL 451 chaff launcher/missile rail (LAU-138)
74 99 99 99 99 74 With EDIT 33, RB 99, Amraam will also be carried
U95 U95 countermeasures pod (almost as Erijammer A110)
AJ/SH SF SK JA
Take off run: 400 m 400 m 400 m 400 m
Landing run: 450 m 450 m 450 m 450 m
Landing speed: 220 km/h 220 km/h 220 km/h 220 km/h
Length: 16.30 m 16.50 m 16.30 m 16.43 m
Span: 10.6 m 10.6 m 10.6 m 10.6 m
Height: 5.6 m 5.6 m 5.6 m 5.9 m
w folded fin: 4.0 m 4.0 m 4.0 m 4.0 m
Engine thrust: 6690 kp 6690 kp 6690 kp 7415 kp
w afterburner: 11790 kp 11790 kp 11790 kp 13125 kp
Range: 2000 km 2000 km 2000 km
Ferry range would be 2250 km, about 15-16% more with Jet A1 fuel.
Empty weight: 9500 kg 9500 kg 9500 kg
Max payload: 3600 kg 2500 kg 1700 kg
(excluding external tank)
Max take off
weight: 18000 kg 17000 kg 18600 kg
Max speed (at 3600 kg load?)
low altitude: Mach 1.1 Mach 1.1 Mach 1.2
high altitude: Mach 2+ Mach 2+ Mach 2+
Guaranteed speed
high altitude: Mach 1.7 Mach 1.7 Mach 1.8
Time from brake release to 10 km or Mach 1 at low altitude: 100 s
Max altitude: 18000 km 18000 m 18000 m
[Air Power Journal, Summer 1993, various issues of FlygvapenNytt
and other Swedish air force informational material]